摘要
目的 研制一种用于机场抢救遇险的高性能战斗机飞行员的救护设备,解决飞机座舱高、救护人员无法登机并快速解救受伤飞行员离机的难题.方法 在勤务需求分析的基础上,提出该救护设备的基本功能要求,论证并设计总体方案,研制出样件.采用qg 0.85拖车底盘,装载自制手控可伸缩旋转的吊臂和可伸缩的登机梯及吊板、吊带.登机梯2架用于救护人员在座舱两侧登机,吊板用于固定受伤飞行员,防止脊柱和颈椎二次受伤.结果 该设备最高牵引速度为80 km/h,展开时间为3～7 min,操作时问为4 min,起吊高度为6 m.结论 该设备适用于机场快速救护,并能在发生事故时为飞行员提供可靠的撤离和保护手段.
objective to develop an airport rescue device for high performance fighter aircraft pilot and to solve such difficulties as carrying the wounded from cockpit by medical staff.methods the basic perfomance specification of rescue device was adopted on the base of analyzing service requirements and the prototype was built upon justification and design.the device was driven by qg 0.85 trailer chassis and equipped with mariusl controlled extendable arm and ladders.as well as assistant safety board and hanging belts.two ladders enabled medical staffs to access cockpit from both sides and assistant ssfety board could be used to protect the spine and cervical vertebrae of wounded pilot from secondary injury. results the 3～7 rnin and evacuation could he completed within 4 min. conclusions the airport rescue device is hdpful in quick rescue mission at airport and provides reliable evacuation and protection to the high performance fighter aireraft pilot in case of accident happened.
出处
《中华航空航天医学杂志》
CSCD
2008年第3期188-192,241,共6页
Chinese Journal of Aerospace Medicine
